Piper PA60-602P Aerostar

Number of Active Aircraft: 67 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 4135 lbs
Max Weight 6000 lbs
Useful Load: 1865 lbs
Engine Name LYC IO-540-S1A5
Engine Number 2
Horsepower 290 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 28000 ft
Max Fuel 165 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 242 kts
GPH (75% BHP): 35
MPG (75% BHP) 6.9
Range (75% BHP): 1006 nm
Fuel Cost Per Seat Mile 0.14 $
Fuel Cost Per Hour 210 $
MPG per 1000 lbs of Payload 12.9
F-T (Speed^2/FuelBurn) 16.7 HP
F-T Payload 31.1 kts
MPH To HP: 8.3 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 2250 ft

SA00024NY Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Amended 10/3/2012
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00082SE Installation of a baggage door strut. Issued 4/29/1994
SA00161BO (1 OF 3) Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00192DE Installation of a Master advisory system (MAS-1) to the existing aircraft annunciator system. Reissued 1/9/1996
SA00243BO (1 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00266DE Gross weight increase from 5500 pounds to 5700 pounds. Amended 10/28/2013
SA00269BO (1OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00290BO (PAGE 1 ) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010
SA00430AT Installation of main landing gear torque links. Issued 3/3/1994
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00505LA Installation of Western Intl Aviation Inc double groove alternator pulley p/n W1A0000A40X-3 on right hand engine and idler pulley p/n W1A000040X-4 on right and left hand engines. Issued 5/22/1998
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (2 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00680SE (6 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00682SE Installation of a sunvisor system. Reissued 3/24/2003
SA00729SE Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760 Revision - dated 7/20/99 or later FAA approved revision. Amended 11/30/2005
SA00749AT Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) Amended 12/10/1997
SA00769CH Installation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540 AEIO-540 and HIO-540 engines. Reissued 2/10/2009
SA00780SE (PAGE 1) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00804SE Installation of an engine failure indicator system also referred to as a low Thrust Detector system.  Amended 7/16/2000
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00943SE Installation of Merlyn Products Inertia Link on the above model aircraft per Merlyn Top Drawing List 91.50-TDL Revision A dated July 13 2001 and Merlyn Installation Instructions Report 91.50-1 Revision N/C dated June 12 2001 or later FAA approved revision of either of these documents. Issued 7/18/2001
SA00944CH Replace Janitrol/JanAero Combustion Heater Model 81D94-X (XX) with C&D Associates Combustion Heater Model CD45K either P/N RA-81D94-3 or P/N CD81D94-3. (95-B55 S/N TC-1658 and up E55 S/N TE-959 TE-968 and up 58 S/N TH-437 and up) Amended 6/20/2000
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01105WI-D (1 OF 2) Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). Amended 5/31/2007
SA01111NY-D Installation of November Whiskey Inc. seat track connectors. Reissued 2/28/2002
SA01147WI Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Reissued 7/30/2012
SA01205WI-D (1 OF 2) Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. );INSERT INTO stc_table VALUES (  Amended 11/20/2007
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (1 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01435DE Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine.  Reissued 5/25/2011
SA01473SE (1 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01511SE Installation of MTV-14-B propellers Issued 2/18/2005
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (1 OF 5) Installation of an antenna Amended 2/15/2007
SA01701SE Allow an increase in the takeoff maximum gross weight of the above model aircraft to 6850 pounds. Amended 11/8/2006
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01786CH Replacement of certain BFGoodrich pneumatic deicer boots per SMR Technologies Inc. Installation Instructions as listed on AML No. SA01786CH or later FAA approved revision. Issued 3/5/2003
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01828SE Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System Reissued 5/12/2011
SA01861SE (PAGE 1)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01933LA-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (1 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006
SA01988SE (PAGE 6) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02024NY Installation of constant speed hydraulically controlled variable pitch 4-blade MTV-14-B-C-F/CF (1) 188-30d propellers. Issued 11/12/2004
SA02033AT (PAGE 1) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. Amended 7/25/2008
SA02085AT Install Aero Crafters engine reheater kit. Issued 3/7/2000
SA02110CH (PAGE 1) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02203AK (PAGE 3)  Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02212AK (PG 1) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems  Amended 5/4/2011
SA02217AK (1 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004
SA02242SE  Fabrication of blended winglets  Amended 3/12/2013
SA02246AT Install propellers MTV-14-B-C-F/CF188-30d 4-blade propeller and spinner assembly. Reissued 11/13/2002
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02268CH (PAGE 1) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02293AK (2 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02547AT (PG 2) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 1) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA03148NY (PAGE 2 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09124AC-D Installation of S-TEC System Two Axis Automatic Flight Guidance System Model ST-606 with optional autotrim system. Amended 11/20/2001
SA09422AC-D Installation of S-TEC Yaw Damper System Model ST-870. Issued 5/10/2000
SA1007NW Installation of a low thrust detector system. Reissued 3/6/1998
SA10236SC (1 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1041GL Install Egan Aviation air ambulance stretcher P/N 125 using Installation Kit P/N 800. Reissued 5/1/1997
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1089CE-D Installation of Collins Radio Group AP-106 autopilot system and inter- face with Collins FD-112 flight director. Amended 3/24/1976
SA1090CE-D Installation of Collins Radio Group AP-107 3-axis autopilot system and interface with Collins FD-112 flight director indicator. Issued 3/24/1976
SA1104CE-D Installation of Collins Radio Group AP-107 2-axis autopilot system and interface with Collins FD-112 flight director indicator. Issued 3/24/1976
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1139SO Installation of a Bendix FCS-870 automatic flight control system. The following options are included: pre-select altitude yaw damper and flight director system. Issued 3/13/1980
SA1174CE Installation of Aero Space Controls Corp. 100 AMP alternator. Issued 10/31/1975
SA1175CE Installation of Aero Space Controls Corp. air conditioning system. Issued 10/31/1975
SA1184CE Installation of King KFC 200 2 axis(3 optional) Flight Control System with King KCS 55 (or -55A) compass and a King KI 255 (or -256) Flight Command Indicator or a KG 258 Attitude Horizon Gyro with a KC 292 Mode Controller. Reissued 2/28/2000
SA1277CE Installation of Avcon Industries stretcher P/N 4001-101 or4001-102. Reissued 8/21/1990
SA1305SO Installation of an adjustable nine- inch trim tab on the left aileron. Amended 1/12/1989
SA1308SW Addition of toilet provision. Reissued 8/25/2005
SA1327GL Install Cabin Door Ajar Warning System. Amended 8/10/1989
SA1338SO Installation of under seat storage container in accordance with Southern Research & Development Drawing No. CA-3000 Revision No. 1 dated April 14 1982 or later FAA approved revisions. Reissued 6/27/2003
SA1347SW Alternate vent for fuel pressure gages. Issued 7/22/1971
SA1356SW Fabricate and install rib-wing fairing-inboard (flap attachment bracket). Issued 8/13/1971
SA1362SW Storage drawers under cabin seats. Issued 9/3/1971
SA1363SW Installation of pressure relief valves in fuel tanks. Issued 9/3/1971
SA1382SW Modify two passenger seats to face aft. Reissued 8/25/2005
SA1391SW Dual hydraulic pump. Issued 11/12/1971
SA1452SW Modfy Ted Smith control tube P/N A600128-3. Issued 3/30/1972
SA1512WE (2 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007 0:00
SA1530CE-D Installation of King KAS 297 altitude selector option in airplanes equipped with KFC 200 Flight Control System with Flight Director installed under STC SA1184CE. Reissued 2/28/2000
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1608NM Installation of an auxiliary fuel tank system. Amended 11/1/1998
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1658NM Installation of engines and propellers with options of intercooler and maximum takeoff weight increase. Amended 1/9/2001
SA1664NM Installation of engine driven air conditioning compressor. Reissued 11/27/2001
SA1675WE Installation of exhaust gas temperature monitoring systems EGT-2. Amended 8/28/1974
SA1720GL Installation of wastegate actuator filter kit. Reissued 9/2/1992
SA1777CE-D Installation of KAP 150 two-axis or KFC 150 two-axis flight control system with optional third (yaw) axis and optional KAP 297B Vertical Speed and Altitude Selector. Reissued 2/28/2000
SA1797SW Mitchell automatic flight system AK459 consisting of Century I auto-pilot with optional omni tracker. Reissued 7/16/1984
SA2121NM Installation of a low pressure fuel boost pump system. Amended 11/1/1998
SA2143NM Installation of Vortex generators fairings rudder seals stall strips and strakes. Amended 11/1/1998
SA2207WE Installation of electrically-driven Freon air-conditioning system Reissued 5/17/2013
SA2336WE Installation of Prestolite 70 amp alternators (Avco Lycoming P/N78314) in lieu of existing 50 amp alternators. Reissued 5/1/1991
SA2346WE Installation of turbocharger overboost protection. Reissued 5/1/1991
SA2357WE Installation of auxiliary hydraulic pump. Reissued 3/10/2009
SA2367WE Installaton of Prestolite 70 amp alternators (Avco Lycoming P/N78314). Reissued 5/1/1991
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2586NM (PAGE 4) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2612NM Installation of fire resistant fuel and oil lines. Amended 11/1/1998
SA2655WE Installation of auxiliary hydraulic pump option. Reissued 5/1/1991
SA2664WE Modification of fuselage structure for pressurization to 3.20 psi operating pressure and installation of pressurization system. Reissued 5/1/1991
SA2693NM (PAGE 2) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009 0:00
SA2714SO Installation of Mallen Aerospace Corp. (MACO) engine turbocharger exhaust Y pipe and turbocharger V clamps. (PA-60-601P (AEROSTAR 601P) TURBOCHARGED ONLY) Issued 3/9/1990
SA2717SO Removal of turbochargers previously installed by STC SE6WE and installing modified exhaust tailpipe. Amended 8/29/1990
SA300CE Installation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO) Amended 5/14/1992
SA3029SW-D Mitchell automatic flight system AK521 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 6/20/1984
SA3030SW-D Mitchell automatic flight system AK522 or AK522RD consisting of Century IV autopilot or Century IV flight director autopilot with optional remotive annuciator panel. Reissued 6/20/1984
SA3033SW-D Mitchell automatic flight system AK455 consisting of Century I autopilot with optional omni tracker. Reissued 8/16/1984
SA3343SW-D Mitchell automatic flight system AK800/FD consisting of Century41/flight director autopilot. Reissued 9/21/1983
SA3370WE Installation of Silver Instruments fueltron IIIG or IIIP digital fuel flow and totalizer system. (PA-60-601P (AEROSTAR 601P) s/n 60-0266-XX and up and those aircraft with previously installed option #108) Issued 6/20/1979
SA3372SW-D Automatic flight system YK877 consisting of yaw damper system. Reissued 8/24/1983
SA3589NM Installation of Machen Inc. intercooler engine as modified by STC SE3590NM optional Hartzell HC-C3YR-2UF/FC8468DB-14 propellers. Amended 11/1/1998
SA35GL Install Cleveland Acft Products wheel and brake conversion kit P/N 199-51. Reissued 10/28/1980
SA3643WE Installation of vertical tail floodlight. Reissued 2/28/1980
SA3719SW Installation of Lycoming IO-540-AA1A5 engines Hartzell HC-CY-2UF/FC-8468/8R propellers and two Ray-Jay 103599-02 turbochargers on each engine to maintain maximum continuous cruise power. (PA-60-601 (AEROSTAR 601) B) Issued 1/6/1987
SA3770WE Installation of Silver Instruments fueltron IIIG or IIIP digital fuel indicating system. Reissued 4/29/1991
SA3862NM Page 2 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA3884WE Installation of cabin door pneumatic spring counterbalance. Reissued 7/15/1988
SA4005NM (PG 1) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4009NM Installation of the Merlyn Products induction air intercooler system on the Piper Aerostars equipped with Lycoming IO-540-AA1A5/-PIA5/-S1A5 engines. Amended 8/16/1989
SA4021NM Installation of Machen temperature monitoring system. Amended 11/1/1998
SA4029WE Installation of Hoskins Model CFS-2000 -2001 or FT-200 fuel flow indicating system. (PA-60-602P (AEROSTAR 602P) Reissued 1/30/1998
SA4144WE Installation of 35 ampere-hour batteries. Issued 5/1/1980
SA4156NM Installation of Meryln Products Inc. Induction Air Intercooler System(STC No. SA4009NM) new Rotomaster ME60 turbochargers and Hartzell HC-C3YR-2UF/FC6660 or HC-C3YR-2UF/ FC8468(D)-8 propeller. Amended 6/27/1994
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4307NM Installation of Hartzell (see STC) propellers and increase in maximum continuous power to 300 HP for existing Lycoming IO-540-K1F5 -K1J5 engines installed on the Model 600 and IO-540-S1A5 engine installed on the 601 and 601P models. Amended 11/1/1998
SA4366NM Installation of Spoilers Inc. electric/hydraulic operated wing Spoiler System. Issued 10/18/1988
SA4367NM Installation of Cleveland Model40-128/30-930 (wheel/brake) assembly. Issued 11/16/1988
SA4389NM Installation of Precise Flight Inc. Series 200 Speedbrake System. Amended 11/7/2003
SA443SO Installation of Bendix RDR-110 weather radar system per Bendix drawing 4009700 Rev. B. Installation of Norton AD4059KX-5 radome approved per STC SA845EA. Issued 9/25/1970
SA444SO Installation of Bendix Model FCS 810 flight control system including flight director indicator DH 841( ). Amended 6/3/1976
SA4472NM Installation of inflatable door seal. Amended 8/18/1983
SA4485NM Installation of FC/FT-10 digital fuel flow indicating system. (PA-60-602P (AEROSTAR 602P) S/N 60-0266-XX AND UP) Issued 6/20/1988
SA4718NM Installation of a pneumatic door seal pressure system. Amended 4/20/1999
SA4724NM Installation of Cleveland brakes. Amended 4/20/1999
SA4777NM Installation of Machen Inc. Oil Breather Separator System. Amended 4/20/1999
SA4790NM Installation of Cleveland slotted brake disks and heavy duty brake linings. Amended 4/20/1999
SA4798NM Installation of an Engine Fire Detection System in each nacelle. Amended 11/1/1998
SA4827NM Installation of exhaust systems. Issued 1/11/1990
SA4942NM Install Lycoming IO-540-AA1A5 or IO-540-S1A5(AE) engine as modified by STC SE4941NM with Rotormaster 600846-01/-02 or600803-01/-02 turbochargers. Issued 5/30/1990
SA4951NM Installation of spoilers. Reissued 7/31/2013
SA4976NM Installation of exhaust system tailpipe redesign. Amended 11/1/1998
SA511GL Installation of a Shadin Model910502 910504 or 910514 fuel flow indicating system. Amended 2/14/1984
SA5133NM Install turbocharger lubrication lines. Issued 3/6/1991
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA5467NM Installation of acrylic window liners. (206 SERIES 402B0301 AND ON) Reissued 1/23/2004
SA5492SW Install auxiliary fuel tank in baggage compartment. Reissued 5/1/1991
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA593CH (1 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009
SA61GL Installation of radome kit P/N 4079KX or 4079X. Amended 10/12/1984
SA693CE Replace existing engine induction air filter with AC Spark Plug filter. Reissued 6/20/2000
SA7160SW-D Installation of S-TEC System 65 two axis automatic flight guidance system with Autotrim Model ST-311. Amended 5/10/2000
SA7168SW-D Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-312 with optional autotrim system. Amended 8/21/2000
SA7204SW-D Installation of S-TEC System 60 Pitch Stabilization System Model ST-454 with Optional Automatic Electric Trim System. Issued 1/26/1990
SA771CE Installation of Woodward propeller unfeathering accumulator kit number213702. Reissued 3/20/1992
SA788WE Mixture monitor (exhaust gas temperature probe and gage). See FAA-approved eligibility list for models. Issued 1/1/1960
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
SA8431SW Installation of R15VON alternator control unit. Amended 1/6/1994
SA845EA Installation of radome kit P/N 4059KX or 4059X. Reissued 9/29/1975
SA8705SW Installation of R25V0N Alternator Control Unit or R2510N Alternator Control Unit or V2510A Over Voltage Sensor. Amended 6/21/1996
SA8922SW Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) Issued 7/21/1994
SA979NW Installation of a Lycoming engine Hartzell propellers Woodward propeller synchrophasers and unfeathering accumlators modified pressuriztion system to 4.25 psi Aero-Air Corporation air conditioning system 35 ampere hour batteries interior sound reduction package aerodynamic performance package and associated systems (See STC for models) Amended 4/10/1981
SA980NW Installation of Lycoming engines Hartzell propellers aerodynamic performance package and associated systems. (See STC for model numbers). Amended 11/1/1998
SA981NW Installation of 35 ampere hour batteries. Amended 11/1/1998
SA982NW Installation of an interior sound reduction package. Amended 11/1/1998
SA983NW Installation of a cabin air conditioner system. Reissued 11/27/2001
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST01468CH Installation of various SMR Technologies electrical propeller deicer models. Amended 7/25/2006
ST01494LA (PG 2) Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. Reissued 8/30/2011
ST02547AT (2 OF 2) Installation of a voice alert system. Amended 5/13/2003
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Limitations
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)